Pratt & Whitney Canada PW206C
Service difficulty reports · 63
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'PW206C' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'PW206C' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2026FA0000821Regulator Valve · faultedHELICOPTER N57HR EXPERIENCED NR 1 OIL HOT LIGHT IN FLIGHT. PER RFM IT SAYS TO ACHIEVE SAFE OEI FLIGHT AND SHUT DOWN ENGINE USING EMERGENCY SHUTDOWN IN AN EMERGENCY. 3-73 AND 3-20 IN RFM. WHICH IS WHAT THE CREW DID.SDR QMLA2024030620028Unknown · odorDURING SHIFT CHANGE CREW REPORTED HAVING SLIGHT FUEL SMELL IN AFT CABIN, PILOT DID NOT REPORT ANY FUEL ODOR IN COCKPIT.SDR QMLA2024021920021Bladder · deterioratedSLIGHT ODOR OF FUEL SMELL REPORTED IN FLIGHTSDR QMLA2023083120068Door · unknownLEFT REAR PASSENGER DOOR OPENED DURING CRUISE FLIGHT. AIRCRAFT WAS SLOWED DOWN TO 25 KTS IN ORDER FOR CREW MEMBER TO ATTEMPT TO CLOSE IT. HE WAS UNABLE TO SLIDE IT CLOSED, AND CONTINUED TO HOLD THE DOOR UNTIL A PRECAUTIONARY LANDING COULD BE MADE. ONCE LANDED SDR U0GA202307072410Lock Nut · crackedWHILE PERFORMING THE POST FLIGHT CHECK IT WAS FOUND THAT THE SWASHPLATE SUPPORT WAS LOOSE AT ITS MOUNTING POINT. UPON FURTHER INSPECTION IT WAS FOUND THAT ALL 6 NUTS WERE WORN AT THE BASE AND 5 OF THE 6 WERE CRACKED. ALL NUTS WERE BACKED OFF APPROX.1.5 TURNS ASDR U0GA ASR8638None · none#1 OIL CHIP CAUTION LIGHT ILLUMINATED. ENGINE SHUT DOWN PER EMERGENCY CHECKLIST. CORRECTIVE ACTION: REPLACED AND FLUSHED #1 ENGINE OIL. INSPECTED #1 ENGINE CHIP DETECTOR, PREFORMED GROUND RUN AND LEAK CHECK OF #1 ENGINE. NO DISCREPANCIES NOTED.SDR FDEA202206251561Engine · failedDURING CLIMBOUT L ENGINE OIL TEMPERATURE CLIMBED INTO THE AMBER BAND (167 DEGREES). ACCOMPLISHED QRH AND OIL TEMP REMAINED HIGH. SHUTDOWN ENGINE IAW WITH QRH INSTRUCTIONS AND LANDED SINGLE ENGINE WITHOUT ISSUE. EMERGENCY DECLARED. AFTER SHUTDOWN L ENG SECSDR QMLA2021040920018Frame · crackedDURING AIRFRAME A5450 INSPECTION, FOUND CRACKS IN STATION 4960 FRAME IN AFT BAGGAGE COMPARTMENT.SDR HDNA2019111800381Engine · crackedWHILE ON FINAL APPROX 200-250 FEET WHEN THE NUMBER 1 ENGINE CHIP AND OIL PRESSURE LIGHT CAME ON CONFORMATION OF THESE INDICATIONS CONFIRMED WITH OIL PRESSURE INDICATION AT 0 PSI. THE #1 ENGINE WAS SECURED, AN EMERGENCY WAS DECLARED WITH A RUN ON LANDING PERFORSDR QMLA2018101618113Chip Detector · activatedXMSN OIL CHIP (YELLOW CAUTION LIGHT) ILLUMINATED IN FLIGHT. IN ACCORDANCE WITH THE RFM SUPPLEMENT PAGES, ATTEMPTED TO EXTINGUISH THE CAUTION LIGHT WITH MOMENTARY ACTIVATION OF THE "CHIP BURNER" SWITCH. CAUTION LIGHT REMAINED ILLUMINATED. IN ACCORDANCE WITH SDR QMLA201808218098Vertical Gyro · inoperativeAIRCRAFT BEGAN TO MAKE LEFT AND RIGHT UN-COMMANDED ROLL INPUTS. THE INPUTS INCREASED IN AMPLITUDE AND RATE OVER THE COURSE OF THE NEXT TWO MINUTES. NO AIRCRAFT CAUTION INDICATIONS CAME ON, ISOLATED THE INPUTS USING SAS SWITCHES, ONCE SAS 2 WAS SWITCHED OFF, TSDR QMLA2017072317070Blower · failedAFTER TAKE OFF DURING CLIMB OUT, THE NR 2 ENGINE OIL TEMP. ROSE TO 120 DEGREES. AND A HIGH OIL TEMP CAUTION LIGHT ILLUMINATED. PILOT STARTED DESCENT AND AFTER LANDING SHUT ENGINE DOWN AND TAXIED TO PARKING LOCATION WITH NO FURTHER DIFFICULTY.SDR QMLA2017050817048Support Frame · crackedTHE PILOTS AFT DOOR POST IS CRACKED AT JUNCTION WHERE THE POST ATTACHES TO THE FLOOR. THE CRACK STARTS ON THE INSIDE AND REACHES AROUND TO THE FRONT SIDE OF THE POST.SDR JBZA201605310001Fire Warning · false activationWITHIN 5 MINUTES OF DEPARTURE, RECEIVED NR 1 ENGINE FIRE WARNING. DECLARED EMERGENCY AND BEGAN APPROPRIATE CHECKLIST. DUE TO CLOSE PROXIMITY TO AIRPORT COMPLETED CHECKLIST THROUGH ENGINE SHUTDOWN. REQUESTED AND RECEIVED NEGATIVE INDICATION OF ANY SIGNS OF FSDR QMLA2015073115064Shaft · shearedDISCOVERED DURING A SCHEDULED MAINTENANCE EVENT THE FOLLOWING DISCREPANCY. WHILE PERFORMING BULLETIN 109EP-1222 & AMC EO-06-6322-EO-452, 200 HOUR INSPECTION OF RIGHT SIDE OIL COOLER BLOWER FAN IMPELLER PLAY MEASUREMENT, HE FOUND THE PULLEY TO BE SLIPPING ON ISDR JBZA20150710001Blade · brokenAFTER PREFLIGHT PLANNING, ACFT DOCUMENT & AIRWORTHINESS INSPECTION & NORMAL STARTS, ACFT DEPARTED. AFTER UNEVENTFUL 1.6 HR FLIGHT, ACFT LANDED, TOOK ON 117 GALS JET A FROM FUEL TRUCK. AFTER APPROX 40 MINUTES, ANOTHER PREFLIGHT & UNEVENTFUL STARTS, DEPARTED PSDR QMLA2015041415028Grip · damagedAIRCRAFT LAST FLOWN, 35 MINUTE FERRY FLIGHT, MONDAY AFTERNOON, 4-13-15. ON TUESDAY APRIL 14TH 2015, AT APPROX 1000 HOURS, THE MECHANICS WERE PERFORMING AN AIRWORTHINESS CHECK ON THE AIRCRAFT, SN 11115. WHILE INSPECTING THE MAIN ROTOR AREA ON THE RT SIDE OF TSDR CA150325003Engine · overtorqued(CAN) ENGINE SUFFERED OVERTORQUE.SDR CA150116002Thrust Reverser · abnormal(CAN) RT THRUST REVERSER LEVER WAS ACCELERATING THE ENGINE BEFORE THE THRUST REVERSER BUCKETS WERE DEPLOYED. DURING TROUBLE SHOOTING THE RH THRUST LEVER INTERLOCK SOLENOID IT WAS DISCOVERED THE ISSUE WAS THE MECHANICAL LOCK FOR THE LEVER. THE LOWER PIVOT POISDR IFJA2014110400001Chip Detector · contaminatedDURING NORMAL CRUISE FLIGHT, THE PILOT RECEIVED A MAIN GEAR BOX CHIP LIGHT, PROCEEDED TO THE NEAREST AIRPORT WITH OUT INCIDENT. AFTER LANDING, THE MECH FOUND A FOUND A SMALL PIECE OF METAL ON THE CHIP DETECTOR, REMOVED THE PIECE OF METAL AND REINSTALLED THESDR CA141103011Unknown · power loss(CAN) LOSS OF POWER, BOTH ENGINES, WHILE DESCENDING TO LAND AT HOSPITAL. AUTOROTATION INITIATED. POWER RESUMED AT 50` ABOVE HELIPAD, UNEVENTFUL LANDING. THIS IS THE SECOND OCCURRENCE ON THIS ACFT.SDR K97A2014F00157Skin · crackedWHEN THE LEFT HORIZONTAL STABILIZER WAS REMOVED FOR ELECTRICAL TROUBLESHOOTING, 7 CRACKS IN THE SHEET METAL WERE FOUND ON THE INBD RIB AND FORE AND AFT SPARS WHERE THEY ATTACH TO THE INBD RIB. CRACKS CANNOT BE SEEN WITH THE STABILIZER INSTALLED. A TORQUE TUBSDR 2A6R20140711001Combustion Liner · crackedDURING 800 HOUR BORESCOPE INSPECTION OF ENG CRACKS WERE FOUND IN THE COMBUSTION CHAMBER LINER ASSEMBLY. REPLACED LINER ASSEMBLY WITH A NEW ONE.SDR 2A6R201407110002Combustion Liner · crackedDURING 800 HOUR BORESCOPE INSPECTION OF ENG CRACKS WERE FOUND IN THE COMBUSTION CHAMBER LINER ASSEMBLY. REPLACED LINER ASSEMBLY WITH A NEW ONE.SDR QMLA2014060514064Unknown · odorIN ROUTE , PILOT SMELLED WHAT HE THOUGHT WAS A STRONG URINE SMELL. HE ASKED THE CREW IF THE PATIENT HAD URINATED & THEY SAID HE HAD NOT. THE PILOT THEN DROPPED THE CREW & DEPARTED SOLO SHOOTING A PRACTICE ILS APPROACH & RETURNED TO PICK UP CREW. UPON RETURNSDR CA140416001Latch · worn(CAN) DURING APPROACH THE CABIN LT DOOR OPENED IN FLIGHT. THE CREW SLOWED THE ACFT DOWN AND CONTINUED WITH THE APPROACH AND LANDED SAFELY. MAINTENANCE REMOVED AND INSPECTED THE DOOR, THE DOOR SAFETY LATCHING MECHANISM WAS REPLACED, THE DOOR WAS ALSO RE-ADJUSSDR CA140401014Manifold · leaking(CAN) DURING CRUISE, THE ACFT EXPERIENCE A HARD ABRUPT YAW AND COCKPIT AVIONIC DISPLAY (CAD) DISPLAYED NR 2 ENGINE FAIL. THE PILOT SHUTDOWN AND SECURED THE ENGINE. DIVERTED AND LANDED WITH NO FURTHER INCIDENT. THE NR 2 FUEL MANIFOLD WAS FOUND TO BE LEAKING ATSDR CA140314001Engine · flamed outTHE PILOT REPORTED THE NR 2 ENGINE FLAMED OUT WHEN TRANSITIONING FROM IDLE TO FLIGHT. A TECH OUTSIDE OF HELICOPTER ADVISED OF WHITE SMOKE FROM ENGINE EXHAUST AT THE MOMENT OF ENGINE FLAMEOUT. SUBSEQUENT TROUBLESHOOTING COULD NOT REPRODUCE THE PROBLEM.SDR S6GA2014F00005Turbine Wheel · damagedPILOT REPORTED NR 1 ENGINE CHIP LIGHT ILLUMINATED AND HEARD NOISE, BROUGHT ENGINE TO IDLE, AS NOISE INCREASED, SHUTDOWN ENGINE. MADE UNEVENTFUL SINGLE ENGINE LANDING AT NEAREST AIRPORT. MX FOUND OIL FILTER BY-PASS BUTTON POPPED, CHIP DETECTOR COVERED WITH PSDR S6GA2013F00000Engine · failedDURING CRUISE FLIGHT, NR 1 ENGINE CHIP LIGHT ILLUMINATED AND HEARD STRANGE NOISE. BROUGHT NR 1 ENGINE TO IDLE. AS NOISE INCREASED, SHUT ENGINE OFF. MADE UNEVENTFUL SINGLE ENGINE LANDING. MX FOUND THAT NR 1 ENGINE OIL FILTER BYPASS BUTTON HAD POPPED. CHISDR CA131007002Engine · making metal(CAN) DURING CRUISE WITH NO PATIENTS ON BOARD, THE ENGINE NR 1 CHIP LIGHT ILLUMINATED AND AN UNUSUAL NOISE WAS HEARD. THE PILOT REDUCED POWER, THE NOISE GOT WORSE, THE PILOT ELECTED TO SHUTDOWN & SECURE THE ENGINE. THE FLIGHT WAS DIVERTED AND AN UNEVENTFUL SSDR K97A2013F00102Lever · groovedTORQUE SHAFT LEVER ASSY IS WORN WHERE RIGID CONNECTING LINK ATTACHES. GROOVE WORN IN TS LEVER ASSY.SDR DT1R20130425003Gear · crackedDURING THE ACCOMPLISHMENT OF AN TECHNICAL BULLETIN BT109EP-128 ON A MAIN GEARBOX; A CROWN GEAR, WAS FOUND TO HAVE A CRACK. THE CROWN GEAR WILL BE REPLACED BY A NEW SUPPORT ASSY.SDR 2013FA0000267Control System · restrictedPILOT COMPLAINED ABOUT LOSS OF TAIL ROTOR CONTROL ON LANDING. CHECKED PITCH CONTROL MECHANISM, RIGGING OF CONTROL RODS AND FOUND NORMAL. USING T/R PITCH RIGGING TOOLS FOUND FULL LT PEDAL DEFLECTION LACKING 4-5 DEGREES FULL TRAVEL. SIDE PANEL CARPET SEEMED TSDR K97A2012F00175Bushing · debondedDURING PRE-FLIGHT CHECK, PILOT COMPLAINED THAT THE TAIL ROTOR PEDALS WERE STIFF. MECHANIC CONFIRMED THIS AND DETERMINED THAT THE TAIL ROTOR HUB ASSEMBLY NEEDED TO BE DISSASEMBLED FOR FURTHER INVESTIGATION. UPON DISSASEMBLY MECHANIC FOUND TEFLON FRICTION WASHESDR CA120924011Blade · damaged(CAN) UPON APPROACH HEARD "SWISHING" SOUND, POWER REDUCED, SOUND WENT AWAY. POST FLIGHT INSPECTION: .3333 OF THE LOWER SURFACE OF THE TRIM TAB IS MISSING.SDR 2012FA0000158Support · wornDURING ACCOMPLISHMENT OF 109EP-112, ENGINE MOUNT INSTALLATION INSPECTION AND RT AND LT V-SHAPED SUPPORTS AND REAR SUPPORT LEGS REPLACEMENT. NR 2 ENGINE INBD MOUNT V-SHAPED SUPPORT, FORWARD LEG HAD LATERAL PLAY. UPON REMOVAL OF MOUNT, MOUNT BOLT WAS FOUND WORSDR QMLA2012030812047Mount · damagedAFTER INSTALLING NR 2 ENGINE, DISCOVERED INBD BI-POD MOUNT LOOSE AT LOWER ENGINE DECK FLOOR. CHECKED NR 1 ENGINE AND DICOVERED IT ALSO WAS LOOSE. SUSPECT DAMAGE TO U-CHANNEL AT STRUCTURE WHERE INBD MOUNTS CONNECT. IN THE PROCESS OF REMOVING ENGINE TO FURTHERSDR CA111215008Bushing · cracked(CAN) WHEN DISASSEMBLED FOR 1200-HR LUBRICATION OF THE THRUST REVERSER LATCHBOX SHOULDER BOLT, PN: 07ND78423-1, QTY 7 OF 8 BUSHINGS, PN: NAS77A4-009, WERE FOUND CRACKED AND/OR SEPARATED.SDR QMLA2011102311103Unknown · odorCREW REPORTED SMELLING FUEL THROUGHOUT THE CABIN APPROX 15 MINUTES INTO FLIGHT. THE ODOR LASTED FOR ABOUT A MINUTE, AND THEN DISAPPEARED. LANDED AT DESTINATION WITHOUT INCIDENT. OPEN BOTH ENGINE COWLINGS AFTER SHUTDOWN TO INSPECT FOR ANY SIGN OF A FUEL LEAKSDR QMLA2011090211090Housing · brokenACFT DEPARTED FOR REVENUE FLIGHT. MX WAS NOTIFIED BY GROUND CREW OF POSSIBLE FUEL ON THE HELIPAD. NOTIFIED PILOT OF PRESSENCE OF FUEL AND ADVISED HIM TO LAND AS SOON AS POSSIBLE. UPON MX ARRIVAL AT ACFT, APPLIED POWER TO NR1 FUEL BOOST PUMP AND NOTICED FUEL LSDR CA110803009Oil System · leaking(CAN) DURING CRUISE, THE PILOT NOTICED THE LOW OIL PRESSURE WARNING LIGHT AND SAW PRESSURE WAS FLUCTUATING. WHEN THE PRESSURE FLUCTUATED DOWN TO 10 PSI THE ENGINE WAS SHUTDOWN. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. INITIAL REPORTS OBSERVED LARGE QUANTISDR CA110711010Fuel Control · failedFLAMEOUT ON GROUND PRIOR TO FLIGHT, THE NR 1 ENG HAD AN UNCOMMANDED SHUTDOWN AS THE OIL PRESSURE INDICATION WAS READING ZERO. THE PROBLEM WAS TRACED BACK TO A CONTAMINATED P3 AIR PASSAGE AT THE MAIN OIL PRESSURE SHUT OFF VALVE. ALL LINES AND PASSAGES WERE CLSDR 1EXA01282011001Blade · debondedON PREFLIGHT INSP, FOUND THE INBD BLADE SPOILER SEPARATED ABOUT 6 INCHES FROM THE OTBD SECTION OF SPOILER, PILOT SAID ON HIS WAY, THAT HE FELT A THAT THE FLIGHT WAS NOT AS SMOOTH, AFTER REACHING DESTINATION, ON INSP OF THE BLADE FOUND THE SEPARATION ON THE BLASDR QMLA2011123111001Unknown · odorTHE PILOT AND MEDICAL CREW ONBOARD THE ACFT ALL SMELLED A STRONG FUEL ODOR SHORTLY AFTER TAKEOFF. THE PILOT IMMEDIATELY RETURNED TO THE HANGAR THAT HE JUST DEPARTED TO HAVE MX LOOK INTO THE PROBLEM. THE MECHANIC TROUBLESHOT THE PROBLEM COULD NOT DUPLICATE ONSDR 2010FA0000850Efi · failedUPON RECEIVING THE EFI, IT WAS TURNED ON AND IT OPERATED NORMALLY FOR ABOUT 2 MINUTES, EXCEPT THE CURRENT DRAW WAS HIGH. AT THE END OF THIS PERIOD, AN ACRID ODOR WAS DETECTED BY THE TECH AND THE TEST WAS STOPPED. THE DEFECT AND ITS ROOT CAUSE IS STILL BEINGSDR NXTA11220Terminal · brokenA BROKEN ELECTRICAL WIRE TERMINAL CARRYING 115 VAC CONTACTED THE GROUND SIDE OF THE GFCI ELECTRICAL OUTLET AND MELTED THE PLASTIC BACK OF THE OUTLET. PILOT NOTICED SMELL AND CREW REPORTED SEEING "VISIBLE VAPOR" IN THE AFT CABIN OF THE AIRCRAFT. PILOT MADE ANSDR CA100203001Engine · power loss(CAN) AFTER TAKEOFF THE ENGINE SUFFERED A DROP IN TORQUE FROM 75 PERCENT TO 68 PERCENT ACCOMPANIED WITH FLUCTUATIONS. THE PILOT SWITCHED TO MANUAL MODE AND THE PROBLEM PERSISTED, THEN HE SWITCHED AGAIN TO AUTOMATIC AND THE TORQUE DROPPED FROM 67 PERCENT TO 58 SDR CA090311006Eec · failed(CAN) PILOT NOTICED NO TQ INDICATION ON RT ENG DURING RESTORATION OF ENG CONTROL TO ITS NORMAL POSITION, AFTER A EEC LIGHT ILLUMINATION. EEC LIGHT WENT OUT, ACFT FUNCTIONED NORMALLY, FLIGHT CONTINUED. ON SHORT FINAL TO HOME BASE, LIGHT CAME ON AGAIN, ACFT LANDSDR CA081125020Engine · making metal(CAN) PILOT REPORTED NR 2 ENG CHIP LIGHT ILLUMINATED AT TOP OF CLIMBOUT, IMMEDIATELY FOLLOWED BY A SURGE AND POWER LOSS. PILOT PREPARED FOR A RUN-ON LANDING. NR 2 ENG WAS SECURED, PASSENGERS WERE BRIEFED AND TRAFFIC AND DISPATCH WERE ALERTED. NR 1 ENG WENT TO
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